WO2010136161A1 - Procédé et dispositif permettant d'introduire un gaz liquide dans un récipient - Google Patents

Procédé et dispositif permettant d'introduire un gaz liquide dans un récipient Download PDF

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Publication number
WO2010136161A1
WO2010136161A1 PCT/EP2010/003133 EP2010003133W WO2010136161A1 WO 2010136161 A1 WO2010136161 A1 WO 2010136161A1 EP 2010003133 W EP2010003133 W EP 2010003133W WO 2010136161 A1 WO2010136161 A1 WO 2010136161A1
Authority
WO
WIPO (PCT)
Prior art keywords
vessel
liquid
receiving line
line
receiving
Prior art date
Application number
PCT/EP2010/003133
Other languages
German (de)
English (en)
Inventor
Holger Bau
Uwe Meyer
Jürgen Glasow
Original Assignee
MAX-PLANCK-Gesellschaft zur Förderung der Wissenschaften e.V.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MAX-PLANCK-Gesellschaft zur Förderung der Wissenschaften e.V. filed Critical MAX-PLANCK-Gesellschaft zur Förderung der Wissenschaften e.V.
Publication of WO2010136161A1 publication Critical patent/WO2010136161A1/fr

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C6/00Methods and apparatus for filling vessels not under pressure with liquefied or solidified gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • F17C2201/0109Shape cylindrical with exteriorly curved end-piece
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/03Orientation
    • F17C2201/032Orientation with substantially vertical main axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05Size
    • F17C2201/056Small (<1 m3)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0391Thermal insulations by vacuum
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0614Single wall
    • F17C2203/0617Single wall with one layer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0639Steels
    • F17C2203/0643Stainless steels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/068Special properties of materials for vessel walls
    • F17C2203/0697Special properties of materials for vessel walls comprising nanoparticles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/014Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/016Noble gases (Ar, Kr, Xe)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/016Noble gases (Ar, Kr, Xe)
    • F17C2221/017Helium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/01Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
    • F17C2225/0146Two-phase
    • F17C2225/0153Liquefied gas, e.g. LPG, GPL
    • F17C2225/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/03Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the pressure level
    • F17C2225/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/04Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by other properties of handled fluid after transfer
    • F17C2225/042Localisation of the filling point
    • F17C2225/046Localisation of the filling point in the liquid
    • F17C2225/047Localisation of the filling point in the liquid with a dip tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/03Dealing with losses
    • F17C2260/035Dealing with losses of fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/05Applications for industrial use
    • F17C2270/0509"Dewar" vessels

Definitions

  • the invention relates to a method for supplying a liquid into a vessel, in particular a method for supplying the liquid into a vessel which has a temperature above the temperature of evaporation of the liquid, such as.
  • a method for supplying a liquid into a vessel which has a temperature above the temperature of evaporation of the liquid, such as.
  • the invention relates to a device for supplying a liquid into a vessel, in particular for supplying liquid gas into a tank or a transport vessel, and to a vessel equipped with such a device.
  • Applications of the invention are particularly in the handling of liquid gases such. As liquid nitrogen or helium.
  • liquid gases for cooling technical equipment.
  • the gases such as liquid helium or liquid nitrogen
  • a storage tank into a thermally insulated vessel, in particular a transport vessel or other, intended for cooling vessel, for. B. transferred to a cooling chamber.
  • the transfer of liquid gas takes place in practice z. B. via a vacuum-insulated transfer line between the storage tank and the thermally insulated vessel.
  • the rigid and non-insulated end of the transfer line ends in the gas space of the vessel below its lid.
  • the object of the invention is to provide an improved method for supplying liquid, in particular liquid gas or low-boiling liquids, into a vessel, with which disadvantages of conventional methods are overcome.
  • the invention is intended to enable in particular
  • the object of the invention is also to provide an improved apparatus for supplying a liquid into a vessel, with the disadvantages of Conventional transfer devices are overcome and in particular a minimization of evaporation losses in the liquid supply allows.
  • the object of the invention is also to provide an improved vessel for holding a liquid, in particular a liquid gas, which overcomes the disadvantages of conventional vessels and which in particular allows uptake of the liquid with minimal loss of material.
  • the invention is based on a first
  • An aspect of the general technical teaching to provide a method for supplying a liquid into a vessel, in which the liquid flows through a transfer line into a receiving line arranged in the vessel.
  • the receiving conduit extends in the vessel in the vertical direction between an upper end open to the surrounding gas space, into which the liquid is passed, and a lower end.
  • liquid is supplied to a vessel at a temperature below the vaporization temperature of the liquid.
  • the liquid (liquified gas or low-boiling liquid) is referred to herein as liquid gas.
  • the invention is based, in a second aspect, on the general technical teaching, to provide a receiving line which is suitable for supplying a
  • Liquid is arranged in a vessel and a tubular body having a first, upper end, which is provided for introducing the liquid, and a second, lower end, which is provided for the discharge of the liquid into the vessel, comprises, wherein the tubular body is formed of a plastic material, in particular a glass fiber reinforced material, and / or stainless steel.
  • the invention is based on the general technical teaching of providing a vessel for receiving a liquid, which is equipped with at least one receiving line according to the invention.
  • the receiving line is provided at the end of the transfer line separate line piece.
  • the transfer line and the receiving line can z. B. be separate components or alternatively interconnected components, wherein in a region between the transfer line and the receiving line pressure equalization with the gas space open to the environment is possible. In this area there is an open exhaust gas discharge.
  • the receiving line represents an open line extension of the transfer line.
  • the receiving line is arranged so that the liquid under the action of gravity, d. H. with a vertical component flows from the top to the bottom of the receiving line.
  • the inventive use of the receiving line for transporting the liquid and its introduction into the vessel has the following advantages.
  • the invention prevents a spraying of the liquid against the inner wall or completely prevented.
  • the rate of evaporation of the liquid is reduced when it is introduced into the vessel, since the liquid can evaporate only on the lateral surface of the receiving line, which is much smaller than that of the inner wall of the vessel, in particular of the poorly heat-conducting glass fiber material.
  • This advantageous effect is also achieved with a receiving line made of stainless steel, since there is no direct connection and thus no significant thermal coupling between the receiving line and the transfer line.
  • the open-top end of the receiving line is adapted for pressure equalization between the transfer line and the open to the environment gas space of the vessel. Due to the pressure equalization at the upper end of the receiving line, irregular flows, in particular vortices or turbulences, are advantageously avoided in the vessel.
  • the upper and lower ends of the open conduit act as dampers.
  • the liquid flows into the vessel without any turbulence, which accelerates the cooling of the inner wall of the vessel and makes the evaporation of e.g. B. is minimized by splashes on the inner wall of the vessel.
  • the inner diameter of the receiving line is selected to be greater than the outer diameter of the transfer line at its upper end.
  • the transfer line protrudes into the upper end of the receiving line, wherein the pressure equalization takes place through the gap between the transfer line and the inner wall of the receiving line.
  • the tubular body in this case has a particularly simple construction.
  • the axial opening is formed by the open lower end of the receiving line.
  • at least one radial opening may be provided at the lower end of the receiving line.
  • the radial opening is provided in the wall of the tubular body in the radial direction, ie perpendicular to the longitudinal extent of the tubular body.
  • the radial opening advantageously offers the possibility that the liquid at the lower end of the receiving line can flow laterally into the vessel and into a liquid bath collecting in it.
  • the receiving line can also be placed on a bottom of the vessel with the at least one radial opening without obstructing the outflow of the liquid into the vessel.
  • the receiving conduit can be arranged in the vessel so that the lower end of the receiving conduit has a distance from the bottom of the vessel. A rapid inflow of the liquid into the barrel would thus result.
  • the vessel and the tubular body of the receiving conduit are preferably a solid composite.
  • the vessel equipped with the tubular body enables the liquid supply according to the invention with a reduced evaporation rate.
  • the tubular body of the receiving conduit may be detachably connected to the vessel.
  • the receiving line can be partially used in various vessels for liquid supply.
  • the receiving line can be releasably secured in a vessel opening.
  • the receiving line can be releasably secured to an inner wall of the vessel. In this case, there may be advantages for improved stability of the receiving conduit in the vessel.
  • the detachable attachment of the receiving line to the vessel further has the advantage that, according to a further variant of the invention, the receiving line can be removed from the latter after the liquid has been fed into the vessel.
  • the tubular body of the receiving line made of a plastic with a thermal conductivity is less than or equal to 0.2
  • Glass fiber reinforced plastic offers advantages in terms of high stability both at room temperature and at the temperature of liquid gases below z. B. - 100 0 C. Furthermore, glass fiber reinforced plastic has a low heat conduction, z. B. approx. 0.2 W / mK, so that the receiving line quickly cools when supplying the liquid and thus evaporation of the liquid in the receiving line can be minimized.
  • the vessel into which the liquid is supplied is preferably a thermally insulated container, such.
  • a thermally insulated container such as a Dewar vessel, a cryotank or a cold chamber.
  • the thermally insulated container is intended to hold a low-boiling liquid, upon the evaporation of which a pressure is built up, in particular for holding liquid nitrogen or oxygen or a liquid noble gas, in particular liquid helium or argon, or a composition thereof.
  • Figure 1 a schematic sectional view of a vessel with a receiving line
  • Figure 2 is a schematic sectional view taken along the line I - I in Figure 1;
  • Figure 3 a schematic sectional view of another
  • Figure 4 different variants of radial openings of receiving lines according to the invention.
  • FIG. 5 shows a schematic illustration of the transfer of a liquid gas from a storage tank into a transport vessel
  • FIG. 6 is a graph illustrating the liquid consumption improved with the invention when transferring liquid helium.
  • FIG. 1 illustrates a transport vessel 10 for liquid helium 1 in a schematic sectional view.
  • a receiving line 30 is arranged, which is adapted to supply the liquid helium 1 in the transport vessel 10.
  • the transport vessel 10 has a thermally insulated vessel wall 11, at the upper end of which a vessel opening 12 and at the lower end of which a vessel bottom 13 is provided.
  • the vessel wall 11 is z. B. shaped so that an ellipsoidal interior is formed with a curved vessel bottom 13.
  • the vessel wall 11 comprises a thermally insulating material. For example, a double-walled construction of the vessel wall 11 made of glass and / or steel is set up with an evacuated wall interior.
  • the transport vessel 10 is for receiving z. B. 150 1 liquid helium at a temperature of - 268 0 C provided.
  • the vessel opening 12 has z. B. a diameter of 20 to 30 cm.
  • the transfer line 20 includes z. B. a flexible stainless steel tube with a thermal insulation.
  • a vacuum insulation or for the supply of liquid HeIi- in the transport vessel 10 may be provided a cooling with liquid or vapor nitrogen.
  • the transfer line 20 with a diameter of z. B. 1 cm to 2 cm is z. B. connected to a storage tank (see Figure 5).
  • the receiving conduit 30 comprises a tubular body 35 which is arranged vertically or at least inclined relative to the horizontal in the transport vessel 10.
  • the tubular body 35 has an upper end 31 and a lower end 32, which are respectively arranged correspondingly in the vessel opening 12 and the vessel bottom 13 adjacent.
  • the tubular body 35 is z. B. from GRP (glass fiber reinforced plastic), PTFE, polyimide or stainless steel. Of the
  • Tube body 35 forms z.
  • B a straight hollow cylinder with an axial length in the range of 50 cm to 100 cm, an outer diameter in the range of 4 cm to 7 cm and a wall thickness less than 1 cm.
  • the implementation of the invention in practice is not limited to these dimensions, but can be varied depending on the specific application and in particular adapted to the dimensions of the transport vessel 10.
  • the upper end 31 of the tubular body 35 is connected to the vessel opening 12 by means of a first fixing device 36.
  • the first fixing device 36 comprises z. B. a plurality of support rods 37 between the outer surface of the tubular body 35 and the inside of the vessel opening 12 (see Figure 2).
  • a free line end 22 of the transfer line 20 projects into the upper end 31 of the tubular body 35.
  • the lower end 32 of the tubular body 35 is connected to the vessel bottom 13 by means of a second fixing device 38 (here simultaneously a table for receiving samples).
  • the second fixing device 38 comprises a support table, which on the
  • Container bottom 13 is fixed and has an opening with holding elements 39 for positive reception of the tubular body 35.
  • FIG. 3 illustrates, in a schematic sectional view, a further embodiment of the invention, in which a dewar vessel 10 for receiving the liquid gas is provided.
  • the de-vessel 10 has a cylindrical interior (corresponding to the rectangular cross-section of Figure 3).
  • the vessel wall 11 and the vessel bottom 13 are z. B. made of stainless steel and / or glass with a vacuum insulation.
  • the vessel opening 12 can be closed with a lid 14 (shown in dashed lines).
  • the receiving conduit 30 comprises the tubular body 35 with the upper end 31 and the lower end 32, which has radial openings 34 for the discharge of the liquid into the interior of the dewar vessel 10.
  • the tubular body 35 is connected to the inner surface of the vessel wall 11. It may be a detachable connection, for. B. using cuffs 15 (shown in phantom) may be provided. Alternatively or additionally, the tubular body with the inner surface of the vessel wall 11 fixedly connected, for. B. glued or screwed.
  • the axial length of the tubular body 35 is selected depending on the application of the invention. Preferably, as shown in Figure 3, it is less than the height of the Dewar vessel.
  • FIG. 4 illustrates, by way of example, various variants of radial outlet openings 34, which may be provided at the lower end 32 of the tubular body 35.
  • the axial lower end of the tubular body 35 can be closed (variants A, B and C) or with an axial Opening 33 (variant D) should be open.
  • variant A a plurality of circular or ellipsenförmi- ger, radial openings 34 is provided, which are distributed in the circumferential direction at the lower end 32 of the tubular body 35 are introduced into the wall of the tubular body.
  • a perforation is provided which encompasses a plurality of point-shaped radial outlet openings 34 in one or more rows.
  • a particularly high liquid passage allows the variant C, in which the radial openings 34 are formed as rectangular windows with intermediate webs 36.
  • variant D shows the combination of slot-shaped radial openings 34 with the axial opening 33 at the lower end 32 of the tubular body 35.
  • FIG. 5 schematically illustrates an exemplary embodiment of the supply according to the invention of a liquid gas 1 from a thermally insulated storage tank 40 into a transport vessel 10.
  • the liquid gas 1 eg liquid nitrogen or helium
  • the transport vessel 10 with the receiving conduit 30 according to the invention is constructed, for example, as shown above in Figure 1.
  • the storage tank 40 comprises a cryostat vessel with a vacuum-insulated vessel wall.
  • the liquid gas 1 is passed via the transfer line 20 (lift), which comprises a flexible pipe connection between the storage tank 40 and the transport vessel 10.
  • the liquid transport takes place under the effect of the vapor pressure formed in the interior of the storage tank 40 above the liquid gas.
  • the throughput through the transfer line 20 is adjustable with the valve 21.
  • the liquid gas 1 flows over the transfer line 20 into the receiving line 30 and from its lower end 32 to the bottom of the transport vessel 10.
  • the open ends 31, 32 of the tubular body 35 allow a pressure equalization between the upper gas volume and the pressure on the already existing liquid column, so that turbulence in the liquid Gas 1 can be minimized or completely suppressed.
  • FIG. 6 shows the helium consumption V (Heii qu ) for several series of experiments 1, 2, 3, ... (abscissa) without (curve A) and with (curve B) of the receiving line according to the invention. Only in the first cooling of the cryostat a high liquid consumption was measured in both cases.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

L'invention concerne un procédé permettant d'introduire un liquide dans un récipient (10) et selon lequel le liquide est introduit dans le récipient par le biais d'une conduite de transfert (20), une conduite de réception (30) étant disposée dans le récipient (10), le liquide étant introduit par la conduite de transfert dans l'extrémité supérieure (31) ouverte de la conduite de réception (30) et ressortant par l'extrémité inférieure (32) de la conduite de réception (30) dans le récipient (10). L'invention concerne, en outre, une conduite de réception (30) conçue pour introduire du gaz liquéfié dans un récipient (10).
PCT/EP2010/003133 2009-05-29 2010-05-21 Procédé et dispositif permettant d'introduire un gaz liquide dans un récipient WO2010136161A1 (fr)

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DE200910023320 DE102009023320B3 (de) 2009-05-29 2009-05-29 Vorrichtungen und Verfahren zur Zuführung eines verflüssigten Gases in ein Gefäß
DE102009023320.2 2009-05-29

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US9494282B2 (en) 2012-01-16 2016-11-15 Bayerische Motoren Werke Aktiengesellschaft Storage container for cryogenic compressed gas having an inlet

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US10738945B2 (en) 2014-11-12 2020-08-11 CleanTech Swiss AG Fitting for liquid gas cylinders and filling method

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